关键词: 超燃冲压发动机;高超声速进气道;超声速燃烧;超燃冲压发动机试验

Abstract: The scramjet research in China in recent years is reviewed.Firstly,studies for hypersonic inlets are reviewed,including issues related to interaction between boundary and shock wave in hypersonic inlet,unstarting/ restarting phenomena,isolator,boundary bleeding for hypersonic inlet,internal/external compression ratio for inlet,inlets with sidewall compression,etc..Secondly,supersonic combustion research is reviewed.Then,investigation for scramjet engine model is summarized.Finally,some comments on the research works are given.

Key words: Scramjet;Hypersonic inlet;Supersonic combustion;Scramjet test.